| 摘要 |
<p>The invention relates to a system and method for modifying and controlling trajectories of spacecrafts during space or air navigation and to modify trajectories of inert bodies moving in space. According to the invention, it is possible to controllably modify the trajectory of controlled, remote-controlled or autonomous spacecrafts moving in space; the trajectory of rockets, missiles and other types of controlled or remote-controlled devices executing an air trajectory from the moment of launching until the moment when they reach their target regardless of the location thereof. This technique involves providing an angular moment to the object or making use of its own angular moment with the purpose of changing the trajectory by applying a force couple perpendicular to said angular moment, the radius thereof being determined by the relationship of the intensities of the angular moment and the force couple.</p> |
